COMPUTATION OF ICE SHAPES ON AN AIRFOIL

2010 ◽  
Vol 40 (3) ◽  
pp. 299-307
Author(s):  
A. A. Nikolsky
Keyword(s):  
2003 ◽  
Vol 40 (6) ◽  
pp. 1212-1215 ◽  
Author(s):  
Heloise Beaugendre ◽  
Francois Morency ◽  
Wagdi G. Habashi ◽  
Pascal Benquet

Author(s):  
Fei Zhang ◽  
Lifen Zhang ◽  
Yundan Li ◽  
Zhenxia Liu ◽  
Pengfei Zhu

One of the reliable methods of studying engine icing is to carry out testing in an icing wind tunnel. Due to the operational limitations of test facility, model-size scaling is adopted. An icing scaling test method for the rotating cone is established based on the dimensional analysis coupled with similarity theory and evaluated by considering the rotating effect. Similarity parameters are determined in the following five aspects: flow field similarity, droplet trajectory similarity, water catch similarity, heat balance similarity, and rotating characteristics similarity. Experimental icing tests have been performed at rime and glaze ice conditions to evaluate the scaling method in a closed-loop icing wind tunnel. Results show that the maximum error between the reference and scale ice shapes occurs at the stagnant point. On the areas apart from this, there is a significantly smaller error. Hence, the scaling test method is proven to be effective and reliable and can provide a theoretical basis for parameter selection of the ice wind tunnel tests.


2019 ◽  
Vol 58 (8) ◽  
pp. 1751-1761 ◽  
Author(s):  
Carl G. Schmitt ◽  
Kara Sulia ◽  
Zachary J. Lebo ◽  
Andrew J. Heymsfield ◽  
Vanessa Przybyo ◽  
...  

AbstractThe terminal velocity (Vt) of ice hydrometeors is of high importance to atmospheric modeling. Vt is governed by the physical characteristics of a hydrometeor, including mass and projected area, as well as environmental conditions. When liquid hydrometeors coalesce to form larger hydrometeors, the resulting hydrometeor can readily be characterized by its spherical or near-spherical shape. For ice hydrometeors, it is more complicated because of the variability of ice shapes possible in the atmosphere as well as the inherent randomness in the aggregation process, which leads to highly variable characteristics. The abundance of atmospheric processes affecting ice particle dimensional characteristics creates potential for highly variable Vt for ice particles that are predicted or measured to be of the “same size.” In this article we explore the variability of ice hydrometeor Vt both theoretically and through the use of experimental observations. Theoretically, the variability in Vt is investigated by analyzing the microphysical characteristics of randomly aggregated hexagonal shapes. The modeled dimensional characteristics are then compared to aircraft probe measurements to constrain the variability in atmospheric ice hydrometeor Vt. Results show that the spread in Vt can be represented with Gaussian distributions relative to a mean. Variability expressed as the full width at half maximum of the normalized Gaussian probability distribution function is around 20%, with somewhat higher values associated with larger particle sizes and warmer temperatures. Field campaigns where mostly convective clouds were sampled displayed low variability, while Arctic and midlatitude winter campaigns showed broader Vt spectra.


Author(s):  
Wei Dong ◽  
JianJun Zhu ◽  
Rui Wang ◽  
Yong Chen

The physical processes involved in ice accretion on the rotating blade are complex. It is important to develop high fidelity numerical method and simulate the icing process on the blade under icing conditions. This paper presents a numerical study on the icing process on the rotating blade. The flow field around the blade is obtained using ANSYS FLUENT. The trajectories of supercooled water droplets and the collection efficiency are calculated by Eulerian approach. Heat and mass balance on the rotating blade surface is taken into account in icing process simulations. The NASA Rotor 67 blade is chosen as the computational model. The collection efficiency on the blade surface is computed and the impingement characteristics are analyzed. The 3D icing accretion on Rotor 67 blade is predicted at design point. The ice shapes of accretion time of 5s, 10s and 15s are simulated and the ice shapes at different span positions of the rotating blade are compared.


2019 ◽  
Author(s):  
Marcus Barth ◽  
Johan Degrigny ◽  
James Brown ◽  
Fatih Tezok ◽  
Richard Lewis ◽  
...  

1994 ◽  
Vol 31 (2) ◽  
pp. 263-270 ◽  
Author(s):  
Jaiwon Shin ◽  
Brian Berkowitz ◽  
Hsun H. Chen ◽  
Tuncer Cebeci
Keyword(s):  

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